# Service difficulty reports: N894UP, cancelled Apr 4, 2018

A list on [N894UP, cancelled Apr 4, 2018](https://openairdocs.org/deregistered/N894UP-2018-04-04.md).

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.

Page 1 of 10 · 455 reports

- [SDR UPS09854259](https://openairdocs.org/sdr/UPS09854259.md): Attach Angle · cracked · Dec 19, 2008 · N894UP · Doug DC873F · Elevator Structure
  > INSPECTION TYPE: SV LT ELEVATOR STA 200.238 DOUBLER ATTACHED ANGLE IS CRACKED AND DENTED, REPAIRED IAW DWG 5700911 AND SRM 51-01-21.
- [SDR UPS08854221](https://openairdocs.org/sdr/UPS08854221.md): Skin · damaged · Dec 14, 2008 · N894UP · Doug DC873F · Fuselage Main, Plate/Skin
  > INSPECTION TYPE:SV EVAL REPAIR DOUBLER INSTALLED AT STATION 161 UPPER SURFACE OF FUSELAGE SKIN JUST AFT OF NOSE RADOME SURVEY SEQUENCE 894-F1-43. REPAIRED IAW DC8 SRM 53-02-0 FIG 001 D SHEET 3.
- [SDR UPS08854006](https://openairdocs.org/sdr/UPS08854006.md): Skin · cracked · Nov 22, 2008 · N894UP · Doug DC873F · Fuselage Main, Plate/Skin
  > INSPECTION TYPE:N/A L1 DOOR HOLD OPEN LATCH AT FS 16 BETWEEN LONGERONS L-15L AND L-16L CRACK AT LOWER AFT CORNER OF PRODUCTION TRIMOUT. THE CRACK AND EXISTING STOP DRILL MEASURES 0.70 INCH LENGTH. COMPLIED WITH EO DC8-5330-31311-A.
- [SDR UPS08853645](https://openairdocs.org/sdr/UPS08853645.md): Skin · unknown · Oct 16, 2008 · N894UP · Doug DC873F · Fuselage Main, Plate/Skin
  > INSPECTION TYPE:SV INSTALL EXTERNAL SKIN DOUBLERS AT STA -88 TO -50 AND -29 TO 7 L21R. INSTALLED DOUBLERS IAW SRM DC-8 53-02-01 FIG 007.
- [SDR UPS08853679](https://openairdocs.org/sdr/UPS08853679.md): Doubler · unknown · Oct 15, 2008 · N894UP · Doug DC873F · Fuselage Miscellaneous Structure
  > INSPECTION TYPE:SV (REPAIR STA -45 LBL 33 DOUBLE FILLER) REPAIR PER DAC DWG SR0830026 REF UPS NRC 188379. REPLACED FINGER AND SPLICE DOUBLERS IAW SR 08530026 REV A.
- [SDR UPS08853654](https://openairdocs.org/sdr/UPS08853654.md): Doubler · unknown · Oct 15, 2008 · N894UP · Doug DC873F · Fuselage Miscellaneous Structure
  > INSPECTION TYPE:SV STA 904 OCTAGON DOUBLER REINSTALL DOUBLER. INSTALLED DOUBLER 51-01-08 AND DALFORT XEA X8-53-298.
- [SDR UPS08853675](https://openairdocs.org/sdr/UPS08853675.md): Rib · cracked · Oct 7, 2008 · N894UP · Doug DC873F · Wing, Rib/Bulkhead
  > INSPECTION TYPE:SV RT WING OUTBOARD L/E LOWER RIB CRACKED AT XFS 835. STOP DRILLED CRACK IAW SRM 57-2-0 DC8. MANUF AND INSTALLED REPAIR IAW DC8 SRM 51-1-8AND SRM DC8 SRM 51-01-20D-0.
- [SDR UPS08853673](https://openairdocs.org/sdr/UPS08853673.md): Rib · cracked · Oct 7, 2008 · N894UP · Doug DC873F · Wing, Rib/Bulkhead
  > INSPECTION TYPE:SV RT WING L/E LOWER RIB CRACKED AT XFS 829. STOP DRILLED CRACK IAW SRM 57-2-0 DC8. FABBED AND INSTALLED REPAIR IAW DC8 SRM 51-03-00-0, AND SRM 51-01-20D-0 DC8.
- [SDR UPS08853676](https://openairdocs.org/sdr/UPS08853676.md): Fastener · deformed · Oct 6, 2008 · N894UP · Doug DC873F · Trailing Edge Flaps
  > INSPECTION TYPE:SV SURVEY SEQUENCE 894-W3-28 LT WING INBOARD FLAP INBOARD EDGE WEB EXT REPAIR DOUBLER HAS 2EA DEFORMED FASTENER. REPLACED FASTENERS IAW DC8 SRM 51-01-21.
- [SDR UPS08853677](https://openairdocs.org/sdr/UPS08853677.md): Skin · misrepaired · Oct 5, 2008 · N894UP · Doug DC873F · Wing, Plate/Skin
  > INSPECTION TYPE:SV RT LWR LEADING EDGE DOUBLER STA XFS 524 NEEDS VALIDATION. DOES NOT MEET CRITERIA APPENDIX H STEP 5. 894-W4-19 AREA PREVIOUSLY REPAIRED & AND ADDED EXTRA ROW OF FASTENERS IAW DC8 SRM 57-2-1 TR 57-95 AND SRM 51-1-21.
- [SDR UPS08853674](https://openairdocs.org/sdr/UPS08853674.md): Stop · missing · Oct 5, 2008 · N894UP · Doug DC873F · Landing Gear Doors
  > INSPECTION TYPE:SV LT FWD NLG DOOR BUFFER STOP MISSING. REPLACED FWD NLG DOOR BUFFER STOP IAW DC8 MM 32-22-01-5.
- [SDR UPS08853650](https://openairdocs.org/sdr/UPS08853650.md): Doubler · unknown · Oct 5, 2008 · N894UP · Doug DC873F · Wing, Plate/Skin
  > INSPECTION TYPE:SV RT UPPER LEADING DOUBLER NEEDS VALIDATION AT STA XFS627 FAIL APP H ST STEP 5 894-W4-12 REPAIRED IAW 57-2-1 AND 51-01-04.
- [SDR UPS08853647](https://openairdocs.org/sdr/UPS08853647.md): Doubler · unknown · Oct 5, 2008 · N894UP · Doug DC873F · Wing, Plate/Skin
  > INSPECTION TYPE:SV RIGHT LEADING EDGE DOUBLER NEEDS VALIDATION AT STA XFS 455 FAILED APPH STEP 5 894-W4-07. REPLACED DOUBLER IAW DC8 SRM 57-2-1 FIG 38.
- [SDR UPS08853636](https://openairdocs.org/sdr/UPS08853636.md): Skin · unknown · Oct 5, 2008 · N894UP · Doug DC873F · Wing, Plate/Skin
  > INSPECTION TYPE:SV RT UPPER LEADING EDGE DOUBLER NEEDS VALIDATION AT STA 325 FAILS APPEN DIX "H" STEP 5 SURVEY SEQ 894-W4-5. REMOVED AND REPLACED REPAIR PER DC 8 SRM 57-2-1 FIG 38 TR 57-85.
- [SDR UPS08853623](https://openairdocs.org/sdr/UPS08853623.md): Skin · misrepaired · Oct 5, 2008 · N894UP · Doug DC873F · Wing, Plate/Skin
  > INSPECTION TYPE:SV RT WING LEADING EDGE LOWER DOUBLER I/B SIDE OF NR 4 PYLON NEED VALIDATION AT STA XFS 500. DOES NOT MEET CRITERIA IN APPENDIX H STEP 5. 894-W4- 32 AREA PREVIOUSLY REPAIRED FEF SRM 57-3-1 T/R 57-83.
- [SDR UPS08853619](https://openairdocs.org/sdr/UPS08853619.md): Skin · misrepaired · Oct 5, 2008 · N894UP · Doug DC873F · Nacelle/Pylon Miscellaneous Structure
  > INSPECTION TYPE:SV RT LOWER LEADING EDGE DOUBLER I/B SIDE NR 3 PYLON AT STA XFS 225 DOES NOT MEET CRITERIA APPENDIX H STEP 5. 894-W4-31 AREA PREVIOUSLY REPAIRED FEF DC8 SRM 57-2-1 TR 57-83 FIG 14A.
- [SDR UPS08853618](https://openairdocs.org/sdr/UPS08853618.md): Structure · misrepaired · Oct 5, 2008 · N894UP · Doug DC873F · Wing Miscellaneous Structure
  > INSPECTION TYPE:SV RT WING LOWER L/E DOUBLER REPAIR NEEDS VALIDATION FOR REPAIR AT STA XFS 747.600. DOES NOT MEET CRITERIA IN APPENDIX H STEP 1 SURVEY SEQ 89 4-W4-17. PREVIOUSLY REPAIRED IAW DC8 SRM 57-2-1 FIG 2H PG 15.
- [SDR UPS08853671](https://openairdocs.org/sdr/UPS08853671.md): Flap · misrepaired · Oct 3, 2008 · N894UP · Doug DC873F · Trailing Edge Flaps
  > INSPECTION TYPE:SV SURVEY SEQUENCE 894-W3-28 LT BS XW5.0 I/B FLAP WEB REPAIR DOES NOT MEET CRITERIA FOR APPENDIX H. FLAP REPLACED ON NR 188423.
- [SDR UPS08853670](https://openairdocs.org/sdr/UPS08853670.md): Flap · misrepaired · Oct 3, 2008 · N894UP · Doug DC873F · Trailing Edge Flaps
  > INSPECTION TYPE:SV RT INBOARD FLAP LOWER I/B EDGE DOUBLER IN STA 0.00 NEEDS VALIDATION, FAILED APPENDIX H STEP 5. REMOVED DOUBLER, FABBED AND INSTALLED NEW DOUBLER IAW DC8 SRM 57-2-05 AND SRM 51-1-21.
- [SDR UPS08853605](https://openairdocs.org/sdr/UPS08853605.md): Skin · misrepaired · Oct 3, 2008 · N894UP · Doug DC873F · Trailing Edge Flaps
  > INSPECTION TYPE:SV SURVEY SEQUENCE 894-W3-21 LT INBOARD FLAP EXTERIOR SURFACE AT STA XW1 05 DOES NOT MEET CRITERIA OF APPENDIX H. FLAP REPAIR MEETS CRITERIA TO BE IAW DC8 SRM 57-02-01-0 FIG 002Q.
- [SDR UPS08853603](https://openairdocs.org/sdr/UPS08853603.md): Skin · misrepaired · Oct 3, 2008 · N894UP · Doug DC873F · Trailing Edge Flaps
  > INSPECTION TYPE:SV SURVEY SEQUENCE 894-W3-20 LT INBOARD FLAP UPPER SURFACE AT STA XW89 DOES NOT MEET CRITERIA OF APPENDIX H. FLAP REPAIR MEETS CRITERIA TO BE IAW DC8 SRM 57-02-01-0 FIG 002Q.
- [SDR UPS08853565](https://openairdocs.org/sdr/UPS08853565.md): Structure · misrepaired · Oct 3, 2008 · N894UP · Doug DC873F · Wing Miscellaneous Structure
  > INSPECTION TYPE:SV, L/E STATION XFS 88 DOUBLER DOES NOT MEET CRITERIA FOR APPENDIX H. REPAIR PREVIOUSLY ACCOMPLISHED PER DC8 73F SRM 57-2-1 FIG 2H CLASS B.
- [SDR UPS08853553](https://openairdocs.org/sdr/UPS08853553.md): Skin · misrepaired · Oct 3, 2008 · N894UP · Doug DC873F · Trailing Edge Flaps
  > INSPECTION TYPE:SV RT FLAP UPPER EXT SURFACE BOILER PANEL DOUBLER REPAIR NEEDS VALIDATION. UPON FURTHER INVESTIGATION REPAIR DOES MEET CRITERIA OF EO DC8-5100-304 18 APPENDIX H STEP 5, NO FURTHER ACTION REQUIRED.
- [SDR UPS08853648](https://openairdocs.org/sdr/UPS08853648.md): Doubler · unknown · Oct 2, 2008 · N894UP · Doug DC873F · Fuselage Miscellaneous Structure
  > INSPECTION TYPE:SV STA-53 TO -89 RBL TO RBL 42 DOUBLER NEEDS VALIDATION FOR REPAIR 894-F 3-11. REPAIRED BY SR08530026 AND SRM 53-2-1.
- [SDR UPS08853651](https://openairdocs.org/sdr/UPS08853651.md): Doubler · damaged · Oct 1, 2008 · N894UP · Doug DC873F · Fuselage Main, Structure
  > INSPECTION TYPE:SV EXT DOUBLER AFT LOWER DOOR CUTOUT BS 50.5 TO 55 L30L TO 1 INCH BELOW L 29L NEED VALIDATION FOR REPAIR. REPAIRED SRM 53-02-00 FIG 13.
- [SDR UPS08853695](https://openairdocs.org/sdr/UPS08853695.md): Doubler · damaged · Sep 30, 2008 · N894UP · Doug DC873F · Fuselage Main, Plate/Skin
  > INSPECTION TYPE:SV BS 659 TO 719.5 L35L TO L35R EXT DOUBLER LOWER BELLY NEED VALIDATION FOR REPAIR. REPAIRED IAW EO DC8-5300-3I587.
- [SDR UPS08853682](https://openairdocs.org/sdr/UPS08853682.md): Doubler · damaged · Sep 30, 2008 · N894UP · Doug DC873F · Fuselage Main, Plate/Skin
  > INSPECTION TYPE:SV EXT DOUBLER BS 1279.5 TO 1299.5 AT L35R CENTERLINE NEED VALIDATION FOR REPAIR REF SEQ 894-FA-57. REMOVED, FABBED AND REPLACED DOUBLER IAW BOEING ROD SKETCH 99-01-20-004 REV IR AND UPS EO DC8-53-20422.
- [SDR UPS08853652](https://openairdocs.org/sdr/UPS08853652.md): Doubler · damaged · Sep 30, 2008 · N894UP · Doug DC873F · Fuselage Main, Structure
  > INSPECTION TYPE:SV EXT WINDOW DOUBLER BS 1400 TO 1421 1.5 ABOVE L14R TO 1.5 BELOW L17R NEEDS VALIDATION FOR REPAIR. REPAIRED BY SRM 51-3-0 AND EO DC 5320-31585.
- [SDR UPS08853599](https://openairdocs.org/sdr/UPS08853599.md): Cusp Web · cracked · Sep 29, 2008 · N894UP · Doug DC873F · Fuselage Miscellaneous Structure
  > INSPECTION TYPE:SV REMOVE AND REPLACE WITH SRM REPAIR. EFN 8941997-55. ORIGINAL N/R 5 34204 LEFT CUSP MEMBRANE CRACKED AT LBL 45 BETWEEN FS 1580-1600. REMOVED DOUBLER VERIFIED CRACK STOP DRILLED IAW SRM 53-02-00-0. REINSTALLED DOUBLER AND VERIFIED REPAIR C
- [SDR UPS08853598](https://openairdocs.org/sdr/UPS08853598.md): Cusp Web · cracked · Sep 29, 2008 · N894UP · Doug DC873F · Fuselage Miscellaneous Structure
  > INSPECTION TYPE:SV REMOVE AND REPLACE EFN 89419971055 ORGINIAL N/R 534204 LEFT CUP MEMBRANE CRACKED AT LBL 45 BETWEEN FS 1580-1600. VERFIED REPAIR COMPLIES WITH SRM 53-02-00 FIG 23.
- [SDR UPS08853585](https://openairdocs.org/sdr/UPS08853585.md): Cusp Web · cracked · Sep 29, 2008 · N894UP · Doug DC873F · Fuselage Miscellaneous Structure
  > INSPECTION TYPE:SV REMOVE REPAIR AND REPLACE WITH SRM REPAIR EFN 89419971080 ORIGINAL N/R 534358 CUSP MEMBRANE CRACKED BETWEEN LIGHTENING HOLES FS 80. UPON INVESTIGATION FOUND REPAIR MISSING ONE ROW OF FASTENERS, ADDED ROW 3 RIVETS AS IAW SRM 53-02-00. FOUN
- [SDR UPS08853568](https://openairdocs.org/sdr/UPS08853568.md): Cusp Web · cracked · Sep 29, 2008 · N894UP · Doug DC873F · Fuselage Miscellaneous Structure
  > INSPECTION TYPE:SV REMOVE AND REPLACE WITH SRM REPAIR ORGINIAL N/R 534146 RIGHT CUSP MEMBRANE CRACK EXTENDING FROM STOP DRILL TO AFT OF FS 1600. INSTALLED DOUBLER AS PER SRM 51-21-01.
- [SDR UPS08853567](https://openairdocs.org/sdr/UPS08853567.md): Cusp Web · cracked · Sep 29, 2008 · N894UP · Doug DC873F · Fuselage Miscellaneous Structure
  > INSPECTION TYPE:SV REMOVE AND REPLACE ORIGINAL N/R 534909 LEFT LOWER CUSP MEMBRANE CRACKED, DENTED AND CORRODED BETWEEN FS 400-420. UPON INVESTIGATION FOUND DAMAGE WAS REMOVED AND VALIDATED REPAIR WAS A ACCOMPLISHED REF DC8 SRM 53-02-00 FIG 25.
- [SDR UPS08853550](https://openairdocs.org/sdr/UPS08853550.md): Rib · cracked · Sep 29, 2008 · N894UP · Doug DC873F · Wing, Rib/Bulkhead
  > INSPECTION TYPE:SV EVALUATION OF N/R 535858 LT WING L/E REPAIR BETWEEN NR 1 AND 2 PYLONS TENTH RIB FROM INBOARD END IS CRACKED. REPAIR WAS ACCOMPLISHED IAW DC8 SRM 57-2-0 SHEET 2 OF 2.
- [SDR UPS08853586](https://openairdocs.org/sdr/UPS08853586.md): Fitting · cracked · Sep 27, 2008 · N894UP · Doug DC873F · Fuselage Miscellaneous Structure
  > INSPECTION TYPE:SV BATH TUBE FITTINGG AT L33R-L34R IS CRACKED. REPAIR AS PER IAW DC8 SRM 51-03-02.
- [SDR UPS08853552](https://openairdocs.org/sdr/UPS08853552.md): Skin · damaged · Sep 26, 2008 · N894UP · Doug DC873F · Fuselage Main, Plate/Skin
  > INSPECTION TYPE:SV FLUSH SKIN REPAIR CUT BS 88 TO 14 BETWEEN L31L AND L27L NEEDS VALIDATION. REPAIR PREVIOUSLY ACCOMPLISHED PER DC8 73F SRM 53-02-01 FIG 007.
- [SDR UPS08853664](https://openairdocs.org/sdr/UPS08853664.md): Skin · damaged · Sep 23, 2008 · N894UP · Doug DC873F · Fuselage Main, Plate/Skin
  > INSPECTION TYPE:SV FUSELAGE EXTERIOR SKIN STA 50 L21R BULGING AND FASTENER HEAD SHEARED. REMOVED FASTENERS STA FS 70 TO FS 50 L19R TO L21R AND FS 50 TO FS 30 IAW DC 8 SRM 51-1-21. REMOVED DOUBLER FROM STA 7 TO STA 70 L20R-L21R. FABBED AND INSTALLED DOUBLER
- [SDR UPS08853661](https://openairdocs.org/sdr/UPS08853661.md): Doubler · gouged · Sep 23, 2008 · N894UP · Doug DC873F · Trailing Edge Flaps
  > INSPECTION TYPE:SV SURVEY SEQ 894-W4-23 RT WING INBOARD FLAP UPPER EXT SURFACE SKIN REPAIR DOUBLER EXT SURFACE GOUGED INBOARD OF BOILER PANEL AT STA XF 211. REMOVED AND REPLACED DOUBLER IAW DC-8 SRM 57-02-05 FIG 2.
- [SDR UPS08853660](https://openairdocs.org/sdr/UPS08853660.md): Doubler · gouged · Sep 23, 2008 · N894UP · Doug DC873F · Trailing Edge Flaps
  > INSPECTION TYPE:SV SURVEY SEQ NO 894-W4-24 RT WING INBOARD FLAP UPPER EXT SURFACE SKIN REPAIR DOUBLER EXT SURFACE GOUGED. REMOVED AND REPLACED DOUBLER IAW DC8 SRM 57-2-05 FIG 2.
- [SDR UPS08853622](https://openairdocs.org/sdr/UPS08853622.md): Repair · corroded · Sep 23, 2008 · N894UP · Doug DC873F · Fuselage Miscellaneous Structure
  > INSPECTION TYPE:SV LOWER FUSE-INT, BATHTUB FITTING REPAIR ANGLE HAS CORROSION AT FS 1180, BETWEEN L33R-L34R JUST INBOARD OF AFT CARGO DOOR CUTOUT LOWER EDGE. REPLACED REPAIR ANGLE IAW DC8 SRM 51-30-00-0-1 AND 53-02-00-0 FIG 002D.
- [SDR UPS08853563](https://openairdocs.org/sdr/UPS08853563.md): Skin · damaged · Sep 23, 2008 · N894UP · Doug DC873F · Fuselage Main, Plate/Skin
  > INSPECTION TYPE:SV FLUSH REPAIR BS 151, 8 INCHES BELOW L21L HAS CLOSE FASTENER SPACING. ACCOMPLISHED IAW DALFORT AVIATION REPAIR XEA X8-53-706 AND REFERENCE DC8-73F SRM 53-2-0 FIG 1C PG 10 10 OF 14.
- [SDR UPS08853667](https://openairdocs.org/sdr/UPS08853667.md): Fastener · loose · Sep 22, 2008 · N894UP · Doug DC873F · Wing, Plate/Skin
  > INSPECTION TYPE:SV SURVEY SEQ NO 894-W3-13 LT WING L/E ABOVE NR 2 PYLON AT XFS 275 SKIN REPAIR DOUBLER HAS 4 FASTENERS LOOSE AND 1 FASTENER PULLED THROUGH. REMOVED AND INSTALLED 5 NEW FASTENERS IAW DC8 SRM 51-3-0 FIG 52A.
- [SDR UPS08853666](https://openairdocs.org/sdr/UPS08853666.md): Fastener · broken · Sep 22, 2008 · N894UP · Doug DC873F · Wing, Plate/Skin
  > INSPECTION TYPE:SV SURVEY SEQ NO 894-W3-01 LT WING L/E LOWER SURFACE SKIN REPAIR DOUBLER HAS 1EA FASTENER HEAD BROKEN AT XFS 404.000 BETWEEN NR 1 AND NR 2 ENG. REPLACED FASTENER IAW UPS DC8 SRM 51-03-00.
- [SDR UPS08853665](https://openairdocs.org/sdr/UPS08853665.md): Skin · misrepaired · Sep 22, 2008 · N894UP · Doug DC873F · Wing, Plate/Skin
  > INSPECTION TYPE:SV SURVEY SEQ NO 894-W3-03 LT WING L/E LOWER SURFACE SKIN REPAIR DOUBLER A HAS 5EA FASTENER HEADS PROTRUDING AT XFS 462.000 AFT OF SLOT DOOR. RE-COUNTERSINK HOLES AND INSTALLED SCREWS IAW DC8 SRM 51-3-0.
- [SDR UPS08853504](https://openairdocs.org/sdr/UPS08853504.md): Skin · damaged · Sep 22, 2008 · N894UP · Doug DC873F · Wing, Plate/Skin
  > INSPECTION TYPE:CV EVALUATION AND DISPOSITION REPAIR SURVEY SEQUENCE NR: 894-W4-09. RIGHT UPPER LEADING EDGE DOUBLER REPAIR STA XFS 512 MISSING 8 EACH FA FASTENERS. INSTALLED FASTENERS IAW DC-8 SRM 51-03-00.
- [SDR UPS08853680](https://openairdocs.org/sdr/UPS08853680.md): Web · corroded · Sep 21, 2008 · N894UP · Doug DC873F · Fuselage Miscellaneous Structure
  > INSPECTION TYPE:SV EVAL AND DISPOSITION REPAIR EFN 89420061026. ORIG NR 994522 L33R STA 1 160 TO STA 1220 UPPER WEB HAS HEAVY CORROSION IN SEVERAL PLACES. REMOVED, FABBED, AND INSTALLED NEW DOUBLER AND FASTENERS IAW REO G12470.
- [SDR UPS08853668](https://openairdocs.org/sdr/UPS08853668.md): Doubler · corroded · Sep 21, 2008 · N894UP · Doug DC873F · Fuselage Miscellaneous Structure
  > INSPECTION TYPE:SV EVAL AND DISPOSITION REPAIR EFN89419971256 ORIG NR 535436 PREVIOUS REPAIR DOUBLER AND TRIPLER ON LONG 33L ARE CORRODED STA 1185-1295. REMOVED AND INSTALLED REPAIR DOUBLER IAW ROD SKETCH 97-05-06-006 AND SRM 51-30-01-00. ACTUAL REPAIR FOUND
- [SDR UPS08853656](https://openairdocs.org/sdr/UPS08853656.md): Web · corroded · Sep 21, 2008 · N894UP · Doug DC873F · Fuselage Miscellaneous Structure
  > INSPECTION TYPE:SV EVAL AND DISPOSITION REPAIR EFN 89419911026. ORIGINAL NR 303033. CORROSION REPAIR TO WEB AND ANGLE AT AFT PASS DOOR FS 1615-1625. REPAIR SATISFIES INTENT AND GUIDELINES OF DC8 SRM 53-2-0 FIG 001D. RF TS 894UP-20-20265.
- [SDR UPS08853655](https://openairdocs.org/sdr/UPS08853655.md): Door Frame · damaged · Sep 21, 2008 · N894UP · Doug DC873F · Fuselage Main, Structure
  > INSPECTION TYPE:SV EVAL AND DISPOSITION REPAIR EFN89419971106 ORIG NR 534710 R-1 DOOR AFT DOOR JAMB REPAIR FOR ELONGATED HOLES (FUSELAGE FRAME). EXISTING REPAIR ACCOMP IAW DWG UPS DC8-53A-011A. RFTS N894UP-12-2027.
- [SDR UPS08853649](https://openairdocs.org/sdr/UPS08853649.md): Door Frame · damaged · Sep 21, 2008 · N894UP · Doug DC873F · Fuselage Main, Structure
  > INSPECTION TYPE:SV EVALUATION AND DISPOSITION EFN 89419971107 ORGINIAL N/R 534711 R-1 DO OF FORWARD DOOR JAMB REPAIR FOR ELONGATED HOLES. REPAIRED BY ANGLE AND WEB REF DC8 51--21 EO DC8 5310-11728B AND DWG 53 DC8 53A-011-REV A.

Next page: https://openairdocs.org/deregistered/N894UP-2018-04-04/reports.md?page=2

## The whole list in SQL

Runs in DuckDB 1.2 or later on the release's Parquet files over HTTPS:

```sql
SELECT sdr_id, difficulty_date, n_number, aircraft_make, aircraft_model, part_name, part_condition, jasc_code, discrepancy
FROM 'https://openairdocs.org/data/latest/faa_service_difficulty_report.parquet'
WHERE n_number = 'N894UP' AND deregistration_id = 'N894UP-2018-04-04'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N894UP-2018-04-04/reports

---
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